Method and assembly for extracting press fit bushings

ABSTRACT

An assembly for removing a bushing is provided including a mandrel having a size and shape similar to the bushing and a receiver having a hollow interior cavity. A fastener extends through an opening formed in both the mandrel and the receiver. A socket attachment has a first opening configured to removably couple to a first end of the fastener and a second opening configured to removably couple to a torque delivery tool. A biasing mechanism arranged adjacent a second end of the fastener is configured to generate a biasing force to drive the mandrel against a bushing in response to a coupling of the socket attachment and the fastener.

CROSS-REFERENCE TO RELATED APPLICATION

The present application is a divisional application and claims priorityto U.S. National Stage Application Ser. No. 15/516,740, filed Apr. 4,2017, which claims priority to PCT Application No. PCT/US15/054413,filed Oct. 7, 2015, which in turn claims priority to U.S. ProvisionalApplication Ser. No. 62/060,671, filed Oct. 10, 2014, the contents ofwhich are incorporated herein by reference.

BACKGROUND OF THE INVENTION

Exemplary embodiments of the invention relate to bushing assemblies, andmore particularly, to a method of removing a bushing assembly from ajoint, such as from a clevis type joints, for example in the main rotorcuff of a rotary wing aircraft.

Clevis type joints, such as used in a rotor blade cuff for example, arecommonly used to transfer a load from one structural member to anotherby a bolt of pin. It may be desirable to bush these clevis joints toprovide protection against damage to the laminated structure which mightoccur such as during bolt installation and/or removal, or due to normalwear. In joints where the loads are transmitted in a direction parallelto the bolt axis, it is frequently desirable to incorporate shouldbushings, which can provide protection for the adjacent surfaces of thejoint.

Bushings are currently removed from a rotor blade cuff using a series ofwashers that damage the cuff, such as by causing surface delaminationsin the structural material of the cuff. As a result of this damage, therotor blade cuff is ultimately scrapped, resulting in significant wasteof both materials and money.

Accordingly, it is desirable to develop a tool and a method of using thetool for removing bushings without damaging the surrounding structure.

BRIEF DESCRIPTION OF THE INVENTION

According to one embodiment of the invention, a socket attachmentincludes a body having a first opening extending inwardly from a firstend of the body and a second opening extending inwardly from a second,opposite end of the body, the first opening being configured to couplethe socket attachment to threads of a fastener and the second openingbeing configured to connect the socket attachment to a torque deliverytool.

In addition to one or more of the features described above, or as analternative, in further embodiments the first opening includes aplurality of threads complementary to a portion of the fastener.

In addition to one or more of the features described above, or as analternative, in further embodiments the second opening differs in atleast one of size and shape from the first opening.

In addition to one or more of the features described above, or as analternative, in further embodiments the torque delivery tool is awrench.

In addition to one or more of the features described above, or as analternative, in further embodiments the torque delivery tool is a socketwrench and the second opening is configured to receive a post extendingfrom a head of the socket wrench.

In addition to one or more of the features described above, or as analternative, in further embodiments the socket attachment furtherincludes a mandrel arranged adjacent a bushing, the mandrel having asize and shape similar to the bushing; a receiver having a hollowinterior cavity; a fastener extending through an opening formed in boththe mandrel and the receiver, the socket attachment being coupled to afirst end of the fastener; and a biasing mechanism arranged adjacent asecond end of the fastener, the biasing mechanism being configured togenerate a biasing force to drive the mandrel against the bushing inresponse to a coupling of the socket attachment and the fastener.

In addition to one or more of the features described above, or as analternative, in further embodiments the biasing mechanism comprises acoil spring.

In addition to one or more of the features described above, or as analternative, in further embodiments the mandrel includes at least onechamfer configured to ensure proper engagement with a bushing.

In addition to one or more of the features described above, or as analternative, in further embodiments the biasing mechanism is positionedbetween a portion of the fastener and the mandrel.

In addition to one or more of the features described above, or as analternative, in further embodiments the biasing mechanism is positionedbetween a portion of the fastener and the receiver.

In addition to one or more of the features described above, or as analternative, in further embodiments the first end of the fastenerincludes a plurality of first threads and the first opening of thesocket attachment includes a plurality of second threads, the pluralityof second threads being complementary to the plurality of first threads

According to another embodiment of the invention, a method of removing abushing, includes installing an assembly, the assembly including amandrel and a receiver positioned on opposing sides of the bushing, asocket attachment, a biasing mechanism, and a fastener extending throughthe mandrel, bushing, biasing mechanism, and receiver; coupling thefastener to the socket attachment; driving the mandrel along an axis ofthe fastener into contact with the bushing; and capturing the bushingwith a hollow interior cavity of the receiver.

In addition to one or more of the features described above, or as analternative, in further embodiments coupling the fastener to the socketattachment compresses the biasing mechanism.

In addition to one or more of the features described above, or as analternative, in further embodiments a biasing force of the biasingmechanism drives the mandrel into contact with the bushing.

In addition to one or more of the features described above, or as analternative, in further embodiments the fastener is threadably coupledto the socket attachment.

BRIEF DESCRIPTION OF THE DRAWINGS

The subject matter, which is regarded as the invention, is particularlypointed out and distinctly claimed in the claims at the conclusion ofthe specification. The foregoing and other features, and advantages ofthe invention are apparent from the following detailed description takenin conjunction with the accompanying drawings in which:

FIG. 1 is a side view of an exemplary rotary wing aircraft embodimentfor use with the present invention;

FIG. 2 is a perspective view of a rotor hub assembly of an aircraftaccording to an embodiment of the invention;

FIG. 3 is a cross-sectional view of an example of a yoke-receiving endof a composite cuff structure of a rotor blade assembly;

FIG. 4 is a perspective view of a yoke-receiving end of a composite cuffstructure including an assembly for removing a portion of a bushingassembly according to an embodiment of the invention;

FIG. 5 is a cross-sectional view of a yoke-receiving end of a compositecuff structure including an assembly for removing a portion of a bushingassembly according to an embodiment of the invention;

FIG. 6 is a perspective view of a yoke-receiving end of a composite cuffstructure including an assembly for removing a portion of a bushingassembly according to an embodiment of the invention;

FIG. 7 is a cross-sectional view of a yoke-receiving end of a compositecuff structure including an assembly for removing a portion of a bushingassembly according to an embodiment of the invention; and

FIG. 8 is a perspective view of a socket attachment tool of the assemblyfor removing a portion of a bushing assembly of FIGS. 4-7 according toan embodiment of the invention.

The detailed description explains embodiments of the invention, togetherwith advantages and features, by way of example with reference to thedrawings.

DETAILED DESCRIPTION OF THE INVENTION

FIG. 1 schematically illustrates an example of a rotary wing aircraft 10having a main rotor assembly 12. The aircraft 10 includes an airframe 14having an extending tail 16 which mounts a tail rotor system 18, such asan anti-torque system, a translational thrust system, a pusherpropeller, a rotor propulsion system, and the like. The main rotorassembly 12 includes a plurality of rotor blade assemblies 22 mounted toa rotor hub 20 assembly. The main rotor assembly 12 is driven about anaxis of rotation A through a main gearbox (illustrated schematically atT) by one or more engines E. Although a particular helicopterconfiguration is illustrated and described in the disclosed embodiment,other configurations and/or machines, such as high speed compound rotarywing aircrafts with supplemental translational thrust systems, dualcontra-rotating, coaxial rotor system aircrafts, tilt-rotors andtilt-wing aircrafts, vertical takeoff and lift rotary wing aircrafts,and fixed wing aircrafts, will also benefit from embodiments of theinvention.

Referring now to FIG. 2, a rotor hub assembly 20 including a hubretention member 24 configured to drive the plurality of rotor bladeassemblies 22 about an axis of rotation A is illustrated in more detail.The rotor hub 24 includes a plurality of radial spokes 26 and shearsegments 28 which structurally interconnect pairs of radial spokes i.e.upper and lower radial spokes 26 a, 26 b, respectively. Each shearsegment 28 in combination with its respective radial spoke 26, forms astructural loop for accepting a rotor assembly yoke 30. The rotorassembly yoke 30 is generally C-shaped and circumscribes, in a loopedfashion, the respective shear segment 28. More specifically, the rotorassembly yoke 30 includes a midsection (not shown) which extends throughthe respective structural loop, and a pair of radial arms (not shown)which project outwardly from the midsection to either side of the shearsegments 28. A composite cuff structure 40 attached to the root end ofeach rotor blade assembly 22 is disposed in combination with the radialarms of a rotor assembly yoke 30.

Referring now to FIGS. 3-7, the composite cuff structure 40 is generallytubular in shape and includes a blade receiving portion 46 adjacent afirst end 42 and a yoke receiving portion 48 adjacent a second, oppositeend 44. The yoke receiving portion 48 is defined by a substantiallyparallel first and second yoke mounting segments 50, 52 having axiallyaligned holes 54 drilled or otherwise formed therein. Each of the yokemounting segments 50, 52 has an unloaded side 56 and a loaded side 58,and the aligned holes 54 are used for positioning a pin P or otherfastener which couples the composite cuff structure 40 to the radialarms 34 of the rotor assembly yoke 30.

To protect the composite cuff structure 40 from damage due to theloading of the pins P, a bushing assembly 60 is positioned within thehole 54 of each yoke mounting segment 50, 52, As shown, the bushingassembly 60 is a shoulder bushing configured to protect not only theinside surface of the holes 54, but also the adjacent loaded andunloaded surfaces of the yoke mounting segments 50, 52 of the compositecuff structure 40. In the illustrated, non-limiting embodiment, thebushing assembly 60 includes a first bushing 62 and a second bushing 64.The first and second bushing 62, 64 may be formed from similarmaterials, or alternatively, may be formed from different materials,such as titanium and brass, respectively, for example.

The first bushing 62 has a substantially cylindrical portion 66 and ashoulder portion 68 which extends outwardly from the cylindrical portion66 as shown in FIGS. 4-7. This first bushing 62 is sized and adapted tobe positioned within holes 54 of the yoke mounting segments 50, 52. Thesecond bushing 64 also has a substantially cylindrical portion 70 and aflange or shoulder 72 extending outwardly therefrom. The cylindricalportion 70 is adapted to fit, such as with a press-fit for example,within the cylindrical portion 66 of the first bushing 62.

Referring now to FIGS. 4-7, an assembly 80 for removing at least aportion of the bushing assembly 60 from within the hole 54 of the yokemounting segments 50, 52 is illustrated in more detail. The assembly 80includes a mandrel 82 having a size and shape generally complementary tothe cylindrical portion 66, 70 of at least one of the bushings 62, 64.In one embodiment, features 86, such as chamfers or perpendicularcutouts with chamfered edges for example, formed in the end 84 of themandrel 82 ensure proper engagement with the bushings 62, 64 and therebyprevent damage to the cuff structure 40 during removal of the bushings62, 64.

The assembly 80 also includes a receiver 88 having a generally hollowcavity 90. The receiver 88 is generally positioned adjacent a surface ofone of the yoke mounting segments 50, 52 such that the receiver 88surrounds the flange 68, 72 of the bushing 62, 64 being removedtherefrom. The receiver 88 is configured to retain the bushing 62, 64within the hollow cavity 90 after being separated from the hushingassembly 60. While shown with a cavity 90, it is understood that otheraspects of the invention do not require a cavity 90 which is closedwhere capture of the bushing 62, 64 is not required.

A fastener 92, such as a bolt for example, extends through a centralopening 93 formed in the mandrel 82 and the receiver 88. A shaft 94 ofthe fastener 92 includes a threaded portion 96 arranged adjacent a firstend 98 thereof. A second opposite end 100 of the fastener 92 may includea head 102 having a diameter larger than the diameter of the adjacentshaft 94. As shown in FIGS. 3-7, the second end 100 of the fastener 92is generally positioned outside of the composite cuff structure 40, suchas vertically above yoke mounting segment 50 for example. A biasingmechanism 104, such as a coil spring for example, is arranged betweenthe head 102 of the fastener 92 and an adjacent component of theassembly 80, such as either the mandrel 82 (FIG. 5) or the receiver 88(FIG. 7).

A socket attachment 106, as shown in more detail in FIG. 8, isconfigured to extend through the hole 54 in the adjacent yoke mountingsegment 50, 52 and engage the threaded portion 96 of the shaft 94. Inone embodiment, the socket attachment 106 has a diameter equal to orsmaller than the pin P. The socket attachment 106 includes a firstinterior hole 112 adjacent a first end 108 and a second interior hole114 adjacent a second, opposite end 110. The size and shape of the firstinterior hole 112 and the second interior hole 114 are generallydifferent. The first interior hole 112 includes a plurality of threads116 generally complementary to the threaded portion 96 of shaft 94. Thesecond interior hole 114 is configured to couple to a portion of atorque delivering tool (not shown), such as the post extending from ahead of a socket wrench for example. As the socket attachment 106rotates, the threaded engagement between the socket attachment 106 andthe fastener 92 causes the head 102 of the fastener 92 to apply a forceto and compress the biasing mechanism 104.

With respect to the embodiment of FIGS. 4 and 5, the assembly 80 isconfigured to drive the second bushing 64 out of a press-fit engagementwith the first bushing 62. The receiver 88 is adjacent flange 72 withinan interior of the cuff structure 40, and the mandrel 82 is positionedoutside the cuff structure 40, adjacent the cylindrical portion 70 ofthe bushing 64, opposite flange 72. The socket attachment 106 extendsthrough the bushing assembly 60 arranged within hole 54 of yoke mountingsegment 52 such that the first end of the socket attachment 106 is indirect or indirect contact, such as via a washer for example, with thereceiver 88. The force applied by the socket attachment 106 on thereceiver 88 limits movement of the receiver out of contact with yokemounting segment 50.

The threaded portion 96 of the fastener shaft 94 is threadably coupledto the socket attachment 106. As the socket attachment 106 is rotated ina first direction, the threaded engagement between the socket attachment106 and the fastener 92 increases. Because the socket attachment 106 isvertically “fixed” relative to yoke mounting segment 50, rotationthereof draws the shaft 94 of the fastener further into the firstinterior hole 112 such that a compressive force is applied to thebiasing mechanism 104. The axial force from the biasing mechanism 104transfers to the mandrel 82 which in turn drives the second bushing 64toward the receiver 88 and out of engagement with the cylindricalportion 66 of the first bushing 62.

FIGS. 6 and 7 illustrate use of the assembly 80 to remove the firstbushing 62 after the second bushing 64 has been removed. In oneembodiment, separate mandrels 82 may be used to remove the first bushing62 and the second bushing 64. For instance, the mandrel 82 used toremove the first bushing 62 may have a slightly larger diameter than themandrel 82 used to remove the second bushing 64. As shown in FIGS. 6 and7, the receiver 88 is arranged at the exterior of the cuff structure 40adjacent flange 68, and the mandrel 82 is arranged within the interiorof the cuff structure 40, adjacent the cylindrical portion 66, oppositeflange 68. The socket attachment 106 extends through the bushingassembly 60 arranged within hole 54 of yoke mounting segment 52 suchthat the first end 108 of the socket attachment 106 is in direct orindirect contact, such as via a washer 120 for example, with the mandrel82.

In the illustrated, non-limiting embodiment, the threaded portion 96 ofthe fastener shaft 94 extends through the mandrel 82 and is threadablycoupled to the socket attachment 106. As the socket attachment 106 isrotated in a first direction, the threaded engagement between the socketattachment 106 and the fastener 92 increases. As a result, the first end108 of the socket attachment 106 drives the mandrel 82 vertically alongan axis of the shaft 94 of the fastener 92, and into contact with thefirst bushing 62. In addition, the biasing mechanism 104 creates areactionary force to the compression force applied thereto by thethreaded engagement between the socket attachment 106 and the fastener92. The reactionary force drives the fastener 92, and therefore thesocket attachment 106 coupled thereto, vertically to displace the firstbushing from the hole 54 of the yoke mounting segment 50.

The assembly 80 illustrated and described herein allows each of thebushings 62, 64 of the bushing assembly 60 to be removed from acorresponding hole 54 without damaging the composite cuff structure 40.The assembly 80 is adaptable such that the orientation of the assembly80 and not the cuff 40 may be changed depending on which bushing 62, 64is being removed. In addition, the socket attachment tool of theassembly 80 provides added benefit by allowing the operator to accessthe fastener 92 through the opposite yoke hole 54. As a result, theprocess of removing the bushings may be performed without heating thebushings, making it convenient for an operator in a hanger or in afield.

While not required, it is understood that aspects of the invention wouldallow press fitting of the bushing 62, 64 through reversal of theassembly 80 to apply the force to the shoulder 72. As such, the assembly80, in aspects of the invention, can be used to both remove and installbushing 62, 64.

While the invention has been described in detail in connection with onlya limited number of embodiments, it should be readily understood thatthe invention is not limited to such disclosed embodiments. Rather, theinvention can be modified to incorporate any number of variations,alterations, substitutions or equivalent arrangements not heretoforedescribed, but which are commensurate with the spirit and scope of theinvention. By way of example, aspects can be used in other contexts fortechnologies using bushings, such as for automotive, maritime, windturbines, industrial machinery, or other technologies where bushings areused. Additionally, while various embodiments of the invention have beendescribed, it is to be understood that aspects of the invention mayinclude only some of the described embodiments. Accordingly, theinvention is not to be seen as limited by the foregoing description, butis only limited by the scope of the appended claims.

What is claimed is:
 1. A socket attachment, comprising: a body having afirst opening extending inwardly from a first end of the body and asecond opening extending inwardly from a second, opposite end of thebody, the first opening being configured to couple the socket attachmentto threads of a fastener and the second opening being configured toconnect the socket attachment to a torque delivery tool.
 2. The socketattachment according to claim 1, wherein the first opening includes aplurality of threads complementary to a portion of the fastener.
 3. Thesocket attachment according to claim 1, wherein the second openingdiffers in at least one of size and shape from the first opening.
 4. Thesocket attachment according to claim 1, wherein the torque delivery toolis a wrench.
 5. The socket attachment according to claim 4, wherein thetorque delivery tool is a socket wrench and the second opening isconfigured to receive a post extending from a head of the socket wrench.6. The socket attachment according to claim 1, further comprising: amandrel arranged adjacent a bushing, the mandrel having a size and shapesimilar to the bushing; a receiver having a hollow interior cavity; afastener extending through an opening formed in both the mandrel and thereceiver, the socket attachment being coupled to a first end of thefastener; and a biasing mechanism arranged adjacent a second end of thefastener, the biasing mechanism being configured to generate a biasingforce to drive the mandrel against the bushing in response to a couplingof the socket attachment and the fastener.
 7. The socket attachmentaccording to claim 6, wherein the biasing mechanism comprises a coilspring.
 8. The socket attachment according to claim 6, wherein themandrel includes at least one chamfer configured to ensure properengagement with a bushing.
 9. The socket attachment according to claim6, wherein the biasing mechanism is positioned between a portion of thefastener and the mandrel.
 10. The socket attachment according to claim6, wherein the biasing mechanism is positioned between a portion of thefastener and the receiver.
 11. The socket attachment according to claim6, wherein the first end of the fastener includes a plurality of firstthreads and the first opening of the socket attachment includes aplurality of second threads, the plurality of second threads beingcomplementary to the plurality of first threads.
 12. A method ofremoving a bushing, comprising: installing an assembly, the assemblyincluding a mandrel and a receiver positioned on opposing sides of thebushing, a socket attachment, a biasing mechanism, and a fastenerextending through the mandrel, bushing, biasing mechanism, and receiver;coupling the fastener to the socket attachment; driving the mandrelalong an axis of the fastener into contact with the bushing; andcapturing the bushing with a hollow interior cavity of the receiver. 13.The method according to claim 12, wherein coupling the fastener to thesocket attachment compresses the biasing mechanism.
 14. The methodaccording to claim 12, wherein a biasing force of the biasing mechanismdrives the mandrel into contact with the bushing.
 15. The methodaccording to claim 12, wherein the fastener is threadably coupled to thesocket attachment.